The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory. Take special note that while the original Bernstein software works with barycentric coordinates, we convert these results into a heliocentric coordinate system.
# Object: 05TV189
# Created Fri Nov 22 02:08:49 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 16.13y
# First observation: 2003/12/16
# Last observation: 2020/01/31
# Chi-squared of fit: 69.02 DOF: 62 RMS: 0.25
# Min/Max residuals: -0.62 0.48
# Exact a, adot, b, bdot, g, gdot:
1.605012E-05 3.211603E-02 -8.165123E-06 -2.197492E-02 3.215880E-02 -1.091990E-03
# Covariance matrix:
2.2171E-13 -4.3912E-14 -4.1026E-14 1.7277E-14 -8.4453E-14 -4.4469E-14
-4.3912E-14 1.3038E-14 1.6241E-14 -6.7884E-15 1.3717E-14 1.8051E-14
-4.1026E-14 1.6241E-14 1.3524E-13 -2.3737E-14 7.2247E-15 3.0062E-14
1.7277E-14 -6.7884E-15 -2.3737E-14 6.9976E-15 -3.2857E-15 -1.2515E-14
-8.4453E-14 1.3717E-14 7.2247E-15 -3.2857E-15 1.0910E-13 5.6934E-15
-4.4469E-14 1.8051E-14 3.0062E-14 -1.2515E-14 5.6934E-15 3.3859E-14
# lat0 lon0 xBary yBary zBary JD0
0.872657 64.395693 -0.323734 0.014182 -0.926633 2452989.815643
# Heliocentric elements and errors
Epoch: 2452990.5000 = 2003/12/17
Mean Anomaly: 354.83619 +/- 0.001
Argument of Peri: 186.23657 +/- 0.002
Long of Asc Node: 246.22164 +/- 0.000
Inclination: 34.37595 +/- 0.000
Eccentricity: 0.19073555 +/- 0.0000
Semi-Major Axis: 39.51553465 +/- 0.0021
Time of Perihelion: 2454291.9212 +/- 7.1
Perihelion: 31.97851724 +/- 0.0022
Aphelion: 47.05255206 +/- 0.0028
Period (y) 248.4048 +/- 0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 13.54129925 +/- 0.0001
Ecliptic Y 29.01763913 +/- 0.0003
Ecliptic Z 0.47332882 +/- 0.0000
Ecliptic XDOT -0.00249787 +/- 0.0000
Ecliptic YDOT 0.00111719 +/- 0.0000
Ecliptic ZDOT -0.00187189 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 32.02522484 +/- 0.0003
Geocenter to KBO 31.09575205 +/- 0.0003
# Hcoef: 7.64
The following table shows the complete astrometric record for 05TV189. The first three columns show the date of observation. The next six columns are RA and DEC. The next column (when provided) is the observed magnitude and filter. The next column is the object name (05TV189) followed by the observatory code and reference code for the source of the astrometry.
2003 12 16.31490 04 08 59.57 +21 52 44.3 22.8g 05TV189 568 Cq9923 2003 12 16.34141 04 08 59.39 +21 52 43.7 22.9g 05TV189 568 Cq9923 2003 12 16.36772 04 08 59.20 +21 52 42.9 22.7g 05TV189 568 Cq9923 2003 12 17.41945 04 08 52.71 +21 52 12.3 05TV189 568 Cq9923 2004 09 12.43791 04 25 17.00 +21 35 37.0 05TV189 695 Cq9923 2004 09 13.47709 04 25 16.57 +21 35 23.3 05TV189 695 Cq9923 2005 10 03.41354 04 33 13.79 +20 32 57.8 05TV189 675 Cq9923 2005 10 03.46371 04 33 13.65 +20 32 56.7 05TV189 675 Cq9923 2005 10 04.38417 04 33 11.08 +20 32 37.9 22.8R 05TV189 675 Cq9923 2005 10 04.43375 04 33 10.93 +20 32 36.7 22.9R 05TV189 675 Cq9923 2005 11 04.43340 04 30 52.30 +20 20 17.6 22. R 05TV189 695 Cq9923 2005 11 04.46770 04 30 52.11 +20 20 16.7 22. R 05TV189 695 Cq9923 2008 09 20.13574 04 58 23.31 +17 38 38.2 23.7R 05TV189 250 S~06Av 2008 09 20.14199 04 58 23.30 +17 38 38.1 05TV189 250 S~06Av 2008 09 20.14893 04 58 23.30 +17 38 37.9 05TV189 250 S~06Av 2008 09 20.20171 04 58 23.28 +17 38 36.8 05TV189 250 S~06Av 2008 12 01.43966 04 53 17.72 +17 08 11.7 22.7R 05TV189 688 C~02Ma 2008 12 01.48483 04 53 17.44 +17 08 10.0 05TV189 688 C~02Ma 2010 01 01.23204 04 58 15.72 +15 55 39.9 05TV189 250 S~0M53 2010 01 01.23442 04 58 15.70 +15 55 39.8 05TV189 250 S~0M53 2010 01 01.23723 04 58 15.69 +15 55 39.8 05TV189 250 S~0M53 2010 01 01.23962 04 58 15.67 +15 55 39.8 05TV189 250 S~0M53 2010 01 01.24470 04 58 15.66 +15 55 40.0 05TV189 250 S~0M53 2010 01 01.25026 04 58 15.62 +15 55 39.9 05TV189 250 S~0M53 2010 01 01.29906 04 58 15.33 +15 55 39.3 05TV189 250 S~0M53 2010 01 01.30462 04 58 15.30 +15 55 39.2 05TV189 250 S~0M53 2011 02 14.382277 05 03 25.536 +14 47 55.31 05TV189 250 S~82m0 2011 02 14.384568 05 03 25.529 +14 47 55.31 05TV189 250 S~82m0 2011 02 14.387288 05 03 25.521 +14 47 55.31 05TV189 250 S~82m0 2011 02 14.389580 05 03 25.514 +14 47 55.30 05TV189 250 S~82m0 2013 11 06.40297 05 36 02.11 +11 57 09.0 21.1R 05TV189 G37 C~0yj0 2013 11 06.48475 05 36 01.70 +11 57 07.1 05TV189 G37 C~0yj0 2020 01 31.310087 06 13 05.160 +04 57 38.68 23.0G 05TV189 T12 C~3iQA 2020 01 31.439113 06 13 04.526 +04 57 40.23 22.7G 05TV189 T12 C~3iQA
The following table shows the residuals to the orbit fit. The first coumn is the point number. The second column is the time, in years, measured from the first observation. The third and fifth columns are the regularized positions used in the orbit fit. The fourth and sixth columns are the residuals, in arc seconds, for RA and Dec respectively.
1 0.0000 0.00 0.05 0.00 -0.54
2 0.0001 0.00 -0.12 0.00 -0.36
3 0.0001 0.00 -0.45 0.00 -0.39
4 0.0030 0.00 0.39 0.00 0.13
5 0.7423 0.00 -0.54 0.00 -0.14
6 0.7451 0.00 -0.62 0.00 0.02
7 1.7990 0.00 0.27 0.00 -0.12
8 1.7992 0.00 0.30 0.00 -0.20
9 1.8017 0.00 0.11 0.00 -0.07
10 1.8018 0.00 0.05 0.00 -0.26
11 1.8867 0.00 -0.03 0.00 0.40
12 1.8868 0.00 0.17 0.00 0.42
13 4.7634 0.00 -0.05 0.00 0.12
14 4.7634 0.00 -0.17 0.00 0.15
15 4.7634 0.00 -0.13 0.00 0.11
16 4.7636 0.00 -0.15 0.00 0.18
17 4.9613 0.00 0.13 0.00 0.44
18 4.9615 0.00 0.48 0.00 -0.16
19 6.0449 0.00 0.13 0.00 -0.12
20 6.0450 0.00 0.04 0.00 -0.18
21 6.0450 0.00 0.13 0.00 -0.14
22 6.0450 0.00 0.05 0.00 -0.10
23 6.0450 0.00 0.35 0.00 0.18
24 6.0450 0.00 0.24 0.00 0.16
25 6.0451 0.00 0.21 0.00 0.32
26 6.0451 0.00 0.25 0.00 0.31
27 7.1651 0.00 0.32 0.00 0.08
28 7.1651 0.00 0.27 0.00 0.08
29 7.1652 0.00 0.22 0.00 0.08
30 7.1652 0.00 0.17 0.00 0.07
31 9.8921 0.00 0.21 0.00 -0.16
32 9.8923 0.00 -0.06 0.00 0.30
33 16.1259 0.00 -0.22 0.00 -0.25
34 16.1263 0.00 -0.19 0.00 -0.32
The following table comes from a 10My integration of the orbit of the object. Three columns are shown. The first column is the result of integrating the nominal orbit. The other two columns are based on clones of the nominal orbit that are +/- 3 sigma from the nominal orbit. If all three types agree then the classificiation is deemed secure. The basis for these calculations is described in more detail in AJ, 129, 1117 (2005). Any use made of these calculations should refer to and credit this publication and the Deep Ecliptic Survey Team.
05TV189 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.738 39.738 39.739 ecceobj 0.195 0.195 0.195 incobj 34.314 34.314 34.314 qmin 31.257 31.257 31.257 qmax 47.948 47.948 47.947 amean 39.454 39.454 39.454 amin 39.121 39.121 39.121 amax 39.813 39.813 39.813 emean 0.155 0.155 0.155 emin 0.092 0.092 0.092 emax 0.207 0.207 0.207 imean 35.904 35.904 35.905 imin 35.056 35.056 35.056 imax 36.706 36.706 36.706 excite_mean 0.607 0.607 0.607 fracstop 1.000 1.000 1.000 cjmean 2.593 2.593 2.593 libcent 0 180.6 180.6 180.6 libamp 0 60.3 60.3 60.3 libcent 1 -180.0 -180.0 -180.0 libamp 1 -180.0 -180.0 -180.0 libcent 2 -180.0 -180.0 -180.0 libamp 2 -180.0 -180.0 -180.0 libcent 3 -180.0 -180.0 -180.0 libamp 3 -180.0 -180.0 -180.0 libcent 4 -180.0 -180.0 -180.0 libamp 4 -180.0 -180.0 -180.0 kozaimean 179.8 179.8 179.8 kozaiamp 179.9 179.9 180.0